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The Rotax 912 was first sold in 1989 in non-certificated form for use in ultralights and motorgliders. [3]The original 60 kW (80 hp) 912 UL engine has a capacity of 1,211 cc (73.9 cu in) and a compression ratio of 9.1:1, and is designed to work with regular automotive gasoline, with up to 10% ethanol.
By 2014, Rotax had produced and sold 50,000 of 912/914 four-stroke engines. [5] Later models increased power, with several variants of the 912 family, and a new 100 kW (135 hp) Rotax 915 iS . [ 5 ] [ 20 ]
The engine can produce rated power up to 15,000 ft (4,572 m) and has a ceiling of 23,000 ft (7,010 m). [1] [2] [6] The engine is based on the Rotax 912, but differs in that it has fuel injection, a reinforced crankshaft, new pistons, a new gearbox and a turbocharger.
EASA type-certified model in the CS-LSA category. Short wing version powered by a 100 hp (75 kW) Rotax 912 S3 engine. [11] Virus SW 600 D Based on the SW 121 but featuring a 100 hp (75 kW) Rotax 912 ULS engine, it is the first aircraft to be certified under the new German LTF-UL2019 rules for the 600 kg microlight category. [22]
Tornado II 912 Two seats in tandem version, intended for the US homebuilt category. It has a 23.5 ft (7.2 m) wingspan. Standard engine is the 80 hp (60 kW) Rotax 912 and cruise speed is 120 mph (193 km/h) with that engine. Acceptable power range is 52 to 80 hp (39 to 60 kW).
It is a high-wing design, mostly using engines from the Rotax 912 family. [1] It was developed from the similar Remos Gemini Ultra. The Mirage has the same layout, landing gear and structure but has a span reduced by 1.00 m (3 ft 3 in), is 170 mm ( 6.7 in) longer and is 34 kg (75 lb) heavier.
The Cavalon is a two-seats-in-side-by-side configuration development of the tandem-seating AutoGyro Calidus.It features a single main rotor, an enclosed cockpit with a complete aerodynamic cockpit fairing, tricycle landing gear with wheel pants and a four-cylinder, air and liquid-cooled, four-stroke, dual-ignition 100 hp (75 kW) Rotax 912 engine or turbocharged 115 hp (86 kW) Rotax 914 or 135 ...
The Calidus features a single main rotor, a two-seats in tandem enclosed cockpit with a complete aerodynamic cockpit fairing, tricycle landing gear with wheel pants and a four-cylinder, air and liquid-cooled, four-stroke, dual-ignition 100 hp (75 kW) Rotax 912 engine or turbocharged 115 hp (86 kW) Rotax 914 engine in pusher configuration.